EP2366910A1 - Einsatz für vibrationsdämpfenden Verschluss - Google Patents

Einsatz für vibrationsdämpfenden Verschluss Download PDF

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Publication number
EP2366910A1
EP2366910A1 EP10250398A EP10250398A EP2366910A1 EP 2366910 A1 EP2366910 A1 EP 2366910A1 EP 10250398 A EP10250398 A EP 10250398A EP 10250398 A EP10250398 A EP 10250398A EP 2366910 A1 EP2366910 A1 EP 2366910A1
Authority
EP
European Patent Office
Prior art keywords
flange
bushing
panel
vibration isolation
hub
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP10250398A
Other languages
German (de)
English (en)
Other versions
EP2366910B1 (fr
Inventor
Manuel Loret De Mola
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Young Engineers Inc
APPLIED CONCEPTS AIRCRAFT SOLUTIONS Inc
Original Assignee
Young Engineers Inc
APPLIED CONCEPTS AIRCRAFT SOLUTIONS Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Young Engineers Inc, APPLIED CONCEPTS AIRCRAFT SOLUTIONS Inc filed Critical Young Engineers Inc
Priority to EP20100250398 priority Critical patent/EP2366910B1/fr
Publication of EP2366910A1 publication Critical patent/EP2366910A1/fr
Application granted granted Critical
Publication of EP2366910B1 publication Critical patent/EP2366910B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F1/00—Springs
    • F16F1/36—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers
    • F16F1/38—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers with a sleeve of elastic material between a rigid outer sleeve and a rigid inner sleeve or pin, i.e. bushing-type
    • F16F1/3807—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers with a sleeve of elastic material between a rigid outer sleeve and a rigid inner sleeve or pin, i.e. bushing-type characterised by adaptations for particular modes of stressing
    • F16F1/3814—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers with a sleeve of elastic material between a rigid outer sleeve and a rigid inner sleeve or pin, i.e. bushing-type characterised by adaptations for particular modes of stressing characterised by adaptations to counter axial forces
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B21/00—Means for preventing relative axial movement of a pin, spigot, shaft or the like and a member surrounding it; Stud-and-socket releasable fastenings
    • F16B21/09—Releasable fastening devices with a stud engaging a keyhole slot
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B5/00—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
    • F16B5/02—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of fastening members using screw-thread
    • F16B5/0216—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of fastening members using screw-thread the position of the plates to be connected being adjustable
    • F16B5/0233—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of fastening members using screw-thread the position of the plates to be connected being adjustable allowing for adjustment perpendicular to the plane of the plates
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B5/00—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
    • F16B5/02—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of fastening members using screw-thread
    • F16B5/0241—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of fastening members using screw-thread with the possibility for the connection to absorb deformation, e.g. thermal or vibrational
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F1/00—Springs
    • F16F1/36—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers
    • F16F1/38—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers with a sleeve of elastic material between a rigid outer sleeve and a rigid inner sleeve or pin, i.e. bushing-type
    • F16F1/3863—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers with a sleeve of elastic material between a rigid outer sleeve and a rigid inner sleeve or pin, i.e. bushing-type characterised by the rigid sleeves or pin, e.g. of non-circular cross-section

Definitions

  • vibrations are transmitted by the structural beams which support the floor panels.
  • These floor panels are typically made of an aluminum honeycomb, or other rigid, lightweight material and vibration causes the panels to vibrate which creates sound. This background sound can be unpleasant and interfere with ordinary conversation, disturb sleep and the like.
  • Other structures or monuments normally found in aircraft interiors such as seats, galleys, bulkheads, etc. supported by the base airframe structure are also subject to vibration and the creation of unwanted sound and noise.
  • a panel assembly having a through hole, at least partially snugly received in said hole a vibration isolation fastener insert comprising:
  • the purpose of the elastomeric bushing is to provide a vibration dampener between the two structural parts.
  • the nut, bolt and seat track do not form part of the invention but do show how the insert is used.
  • the upper housing 20, lower housing 22 having external male threads, elastomeric bushing 24, hub 26 are pre-assembled with the external flange 27 on hub 26 being received in slot 25 in elastomer bushing 24 and the so sub-assembly threaded into the female threads on upper flange 16.
  • the elastomer can be over-molded onto hub 26 whereby the holes on hub are used for anti-rotation and increased bonding surface for the elastomer.
  • a nut 28 and bolt 30 are inserted and made up to join the panel 14 to the structural track 32.
  • FIG. 2a, 2b and 2c of 2 the drawings, in this embodiment the upper flange 116 and the lower flange 118 are press fit, screwed or swaged to each other and capture components.
  • the elastomeric bushing 124 and hub 126 (elastomer/metal hub assembly) are positioned as shown.
  • the dimensions and materials for flange 116 and flange 118 will depend on the type and size of fasteners (e.g., screw, anchor, etc.) used to secure the monument to the vehicle structure and the material into which it will be installed.
  • Hub 126 is to be cylindrical in shape with a circular "T" flange 127 intersecting the cylinder.
  • the flange 127 component on hub 126 are larger than the clearance hole openings on flanges 116 and 118 such that it is retained if pulled axially, even if elastomeric bushing 124 would fail.
  • Hub 126 may be threaded internally to accept any size screw or it can remain unthreaded or through-drilled to act as a bushing, either with/without a countersink on either end to accommodate a flat-head screw.
  • Hub 126 may also be threaded externally at its exposed end to accept adapters of different sizes. The diameter dimensions and finishes of hub 126 may vary to accommodate various size screws, and to accommodate strength requirements.
  • Elastomeric bushing 124 may have ribs or projections 130 to provide anti-rotation elements which can engage slots 128.
  • flange 116 may have an anti-rotation knurled ring or area 133.
  • the assembly can be secured by anti-rotation hex nut 135.
  • This invention lends itself to include the development of a family of insert types that will address many applications and uses.
  • This family of inserts may be viewed in two general categories: Potted Isolator Inserts and swaged Isolator Inserts.
  • the Potted Isolator Insert category would typically be installed through a honeycomb panel attached to (or part of) the monument, and would be secured via the application of a potting compound in the panel cavity surrounding the installed insert and possibly via bonding to flanges of components 116 and 118.
  • the swaged Isolator Insert embodiment would typically be installed in a panel attached to (or part of) the monument by crimping its outer flange(s) after the Insert is installed in a receiving hole on the panel.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Health & Medical Sciences (AREA)
  • Child & Adolescent Psychology (AREA)
  • Vibration Prevention Devices (AREA)
  • Connection Of Plates (AREA)
EP20100250398 2010-03-05 2010-03-05 Insertion de fixation d'isolation contre les vibrations Active EP2366910B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EP20100250398 EP2366910B1 (fr) 2010-03-05 2010-03-05 Insertion de fixation d'isolation contre les vibrations

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP20100250398 EP2366910B1 (fr) 2010-03-05 2010-03-05 Insertion de fixation d'isolation contre les vibrations

Publications (2)

Publication Number Publication Date
EP2366910A1 true EP2366910A1 (fr) 2011-09-21
EP2366910B1 EP2366910B1 (fr) 2012-11-28

Family

ID=42543443

Family Applications (1)

Application Number Title Priority Date Filing Date
EP20100250398 Active EP2366910B1 (fr) 2010-03-05 2010-03-05 Insertion de fixation d'isolation contre les vibrations

Country Status (1)

Country Link
EP (1) EP2366910B1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102021118198A1 (de) 2021-07-14 2023-01-19 Deutsches Zentrum für Luft- und Raumfahrt e.V. Verfahren zum Einsetzen eines Inserts sowie Fertigungsanordnung und Insert hierzu

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5876023A (en) 1996-09-18 1999-03-02 Lord Corporation Vibration isolation insert for aircraft floor planels and the like
US6065742A (en) 1996-09-13 2000-05-23 Lord Corporation Multi-directional tuned vibration absorber
US6138980A (en) 1999-06-24 2000-10-31 Lord Corporation Pilot mounting
US6216833B1 (en) 1999-07-22 2001-04-17 Bridgestone/Firestone, Inc. Vibration damper and method of making same
US6394432B1 (en) 1998-06-10 2002-05-28 Lord Corporation Vibration and/or shock absorbing devices and compensator elements utilized therein
US20020079630A1 (en) * 2000-07-21 2002-06-27 Lord Corporation Vibration isolation device with load dependent stiffness
US6443679B1 (en) 1999-11-23 2002-09-03 Schwarz Verbindings-Systeme Gmbh Vibration-damping connecting arrangement for the detachable connection of two components with a releasing part, which can be moved on a bolt guided by a bush
US7131786B2 (en) 2001-07-20 2006-11-07 Enidine Gmbh Process and device for the damping of motion between two cylindrical parts sliding with one another in translation and friction
US7179039B2 (en) 2002-11-26 2007-02-20 Schwarz Verbindungs-Systeme Gmbh Vibration-damping ring insert arrangement and component connection arrangement incorporating the same

Patent Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6065742A (en) 1996-09-13 2000-05-23 Lord Corporation Multi-directional tuned vibration absorber
US5876023A (en) 1996-09-18 1999-03-02 Lord Corporation Vibration isolation insert for aircraft floor planels and the like
US5876024A (en) 1996-09-18 1999-03-02 Lord Corporation Vibration isolation insert for aircraft floor panels and the like
US6394432B1 (en) 1998-06-10 2002-05-28 Lord Corporation Vibration and/or shock absorbing devices and compensator elements utilized therein
US6138980A (en) 1999-06-24 2000-10-31 Lord Corporation Pilot mounting
US6216833B1 (en) 1999-07-22 2001-04-17 Bridgestone/Firestone, Inc. Vibration damper and method of making same
US6443679B1 (en) 1999-11-23 2002-09-03 Schwarz Verbindings-Systeme Gmbh Vibration-damping connecting arrangement for the detachable connection of two components with a releasing part, which can be moved on a bolt guided by a bush
US20020079630A1 (en) * 2000-07-21 2002-06-27 Lord Corporation Vibration isolation device with load dependent stiffness
US6715746B2 (en) 2000-07-21 2004-04-06 Lord Corporation Vibration isolation device with load dependent stiffness
US7131786B2 (en) 2001-07-20 2006-11-07 Enidine Gmbh Process and device for the damping of motion between two cylindrical parts sliding with one another in translation and friction
US7179039B2 (en) 2002-11-26 2007-02-20 Schwarz Verbindungs-Systeme Gmbh Vibration-damping ring insert arrangement and component connection arrangement incorporating the same

Also Published As

Publication number Publication date
EP2366910B1 (fr) 2012-11-28

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